Part Details | RECEPTACLE DUMMY CONNECTOR
5935-00-880-7001 An item specifically designed to mate with a plug connector to perform one or more special functions, such as to support a plug connector when not in use, short contacts, or open or close electrical circuits, in or on another connector. It does not have provisions for attaching a wire, cable, or contact. It is designed to mount on a panel, bulkhead, wall, or chassis. It does not include connector shells which are merely used to position a plug connector on a panel.
Alternate Parts: 10263999223, 10-263999-223, VG95328T07C22, 850024, 8500-24, VG95328T07C22, KPT1522A, KPT15-22A, MILC26482, MIL-C-26482, MS311522W, MS3115-22W, MS311522A, MS3115-22A, 9.51 02 PR 22, 5935-00-880-7001, 00-880-7001, 5935008807001, 008807001
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-880-7001 | 15092 ( DUMMY CONNECTOR, RECEPTACLE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5935-00-880-7001
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10-263999-223 | D8311 | AMPHENOL-TUCHEL ELECTRONICS GMBH |
| VG95328T07C22 | D9477 | BUNDESAMT FUER AUSRUESTUNG, |
| 8500-24 | D9422 | FCI DEUTSCHLAND GMBH |
| VG95328T07C22 | A6854 | GLENAIR ITALIA SPA |
| KPT15-22A | D1371 | ITT CANNON GMBH |
| MIL-C-26482 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MS3115-22W | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS3115-22A | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 9.51 02 PR 22 | C0062 | TE CONNECTIVITY GERMANY GMBH |
Technical Data | NSN 5935-00-880-7001
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 0.650 INCHES NOMINAL |
| OVERALL HEIGHT | 1.703 INCHES NOMINAL |
| OVERALL WIDTH | 1.703 INCHES NOMINAL |
| CENTER TO CENTER DISTANCE BETWEEN MOUNTING FACILITIES PARALLEL TO HEIGHT | 1.375 INCHES NOMINAL |
| DISTANCE BETWEEN CENTERLINES OF MOUNTING FACILITIES PARALLEL TO BODY WIDTH | 1.375 INCHES NOMINAL |
| DISTANCE FROM MOUNTING SHOULDER TO FRONT FACE | 0.556 INCHES MINIMUM AND 0.587 INCHES MAXIMUM |
| UNTHREADED MOUNTING HOLE DIAMETER | 0.120 INCHES NOMINAL |
| CONNECTOR LOCKING METHOD | BAYONET PIN |
| SHELL TYPE | SOLID |
| SHELL MATERIAL | ALUMINUM ALLOY |
| SHELL SURFACE TREATMENT | CADMIUM |
| SHELL SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE |
| MATING END QUANTITY | 1 |
| ENVIRONMENTAL PROTECTION | MOISTURE RESISTANT AND SALT WATER RESISTANT AND VIBRATION RESISTANT |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| TEST DATA DOCUMENT | 81349-MIL-C-26482 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |
| SPECIFICATION/STANDARD DATA | 96906-MS3115 GOVERNMENT STANDARD |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | FMS-A7 AIRCRAFT; F4S AIRCRAFT; AIRCRAFT, ORION P-3; HELICOPTER, CARRIER BASED ASW, SH-60F; AIRCRAFT, STRATOFORTRESS B-52; AIRCRDAFT, F-16; GUIDED MISSILE, INTERCEPT; AIRCRAFT, EAGLE F-15; AIRCRAFT, THUNDERBOLT II, A-10 |